Archiwa kategorii: SAMOLOTY

IL-76T

Sale IL-76T, YOM 1980, TSN: 12400h, Land.: 4150, Engines: 4xD-30KP-2, load 48.000kg,

TCAS-II  - CAS-67A With Change 7.1 „Allied Signal” „Honeywell”

EGPWS – МFI А813-0409

RVSM – SVS 1-72-1В-76М , UVК-1FPB  and SSVE-МPB-М

GPS  – KLN-90B  „Bendix King”

ELT-406 «АRМ-406P» и «АRМ-406АS1»

Кurs МP-2 , UКV-CМ

Engines:       D-30КP-2                     

1) TSN 4290 cykl. 1570  ,   TSOH  285 cykl 78

2)  TSN 6980 cykl. 1900   , TSOH  3000 cykl 780

3)TSN 7320 cykl. 2015 , TSOH 2330 cykl 545

4)TSN 8200 cykl. 2250  , TSOH 2725 cykl 835

IL-76T out_1IL-76T out_2IL-76T out_5IL-76T out_6

IL-76TD

Sale IL-76TD, YOM 1988, TSN: 6250h, Land.: 2580, Engines: 4xD-30KP-2, load 50.000kg,

TCAS-II  - CAS-67A With Change 7.1 „Allied Signal” „Honeywell”

EGPWS – МFI А813-0409

RVSM – SVS 1-72-1В-76М , UVК-1FPB  and SSVE-МPB-М

GPS  – KLN-90B  „Bendix King”

ELT-406 «АRМ-406P» и «АRМ-406АS1»

Кurs МP-2 , UКV-CМ

Engines:  4x D-30КP-2            

1) TSN 4690 cykl. 1370 , TSOH  2800 cykl 700

2) TSN 7630 cykl. 2170 , TSOH  3040 cykl 670

3) TSN 8200 cykl. 1370 , TSOH 2140 cykl 990

4) TSN 3650 cykl. 1490 , TSOH 1680 cykl 300

78785 (1)Грузовая кабина (вид по полету)Грузовая кабина (погруз. оборуд.)Кабина экипажа (1)

AN-12BK

Technical specification of the aircraft An-12 BK

 

Factory number Date of issue Date of last overhaul Since new Since overhaul

1972г.

2th overhaul

1997

7661h.

5422 land.

4568h.

1710 land.

Engines АI-20M

1st

1969

2001

10125h.

3947h.

2nd

1968

2001

11493h.

3946h.

3rd

1969

1993

8723h.

4163h.

4th

1971

2001

10332h.

        3947h.

 

TG-16M

1977

2006

451h

125h

 

1.Radio communication equipment:

- Radio station „BAKLAN-20D” (2 ps)

- Radio station „Micron”

- Emergency radio station R-855

-Radio station „KOMAR” (2 ps)

2. Radio engineering means of navigation and landing:

- Equipment of navigation and landing КURS-МP-2 (2 ps)

- Plane range finder SD-67

- Automatic radio compass ARK-11 (2 ps)

- Radio altimeter RV-5MD

- Respondent international SОМ-64

- Dopler indication system of speed and drift angle DISS-013-12М

3. The radio navigating equipment:

- Radar station ROS-1

- System GPS-195-2ps

4. Equipment of registering of emergency conditions:

- Onboard system of registration of modes of flight МSRP-12

- Onboard tape recorder MS-61B (2 ps)

- Self-recorder К3-63

5.  Piloting – navigation equipment:

- Course system KS-6G

- Gyro horizon AGD-1S (3 ps)

- Automatic machine of angles of attack and overloads АUАSP-6R

- Giro semicompas GPK-52

- System of direct management «Drive АNP» (the dual complete set)

- Autopilot АP-28D1

6. Installed on the plane in addition:

- Altimeter VMF-50K (in feet)

- Altimeter VAМ-72М.

- Altimeter UVID-15 F

P1030528 — kopiaP1030530 — kopia

AN-12B

Technical specification of the aircraft An-12 BK

Date of issue Date of last overhaul Since new Since overhaul

31.07.1964г.

7th overhaul

1999

28300h.

13723 land.

6900h.

2600 land.

Engines АI-20M

1st

1975

2006

11200h.

1140h.

2nd

1970

1996

18790h.

7400h.

3rd

1993

2003

5560h.

5230h.

4th

1973

1996

16670h.

        7930h.

Рropellers

1-st

1984

2006

7400h

882h

2-nd

1984

2003

6950h

1040h

3-rd

1979

2006

6080h

882h

4-th

1984

20.12.2006

2450h

850h

ТG-16М

         1981 2008       2200h          73h

 

1.Radio communication equipment:

- Radio station „BAKLAN-20D” (2 ps)

- Radio station „Micron”

- Emergency radio station R-855

-Radio station „KOMAR” (2 ps)

2. Radio engineering means of navigation and landing:

- Equipment of navigation and landing КURS-МP-2 (2 ps)

- Plane range finder SD-67

- Automatic radio compass ARK-11 (2 ps)

- Radio altimeter RV-5MD

- Respondent international SОМ-64

- Dopler indication system of speed and drift angle DISS-013-12М

3. The radio navigating equipment:

- Radar station ROS-1

- System GPS-195-2ps

4. Equipment of registering of emergency conditions:

- Onboard system of registration of modes of flight МSRP-12

- Onboard tape recorder MS-61B (2 ps)

- Self-recorder К3-63

5.  Piloting – navigation equipment:

- Course system KS-6G

- Gyro horizon AGD-1S (3 ps)

- Automatic machine of angles of attack and overloads АUАSP-6R

- Giro semicompas GPK-52

- System of direct management «Drive АNP» (the dual complete set)

- Autopilot АP-28D1

6. Installed on the plane in addition:

- Altimeter VMF-50K (in feet)

- Altimeter VAМ-72М.

- Altimeter UVID-15 F

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FOKKER-100

Aircraft Specification
Type & Model:                                       FOKKER 100
YOM:                                                          1991
Passenger:                                                 105
 Airframe Status 30.Dec.2015
Total Airframe Hours:                           51.759 Flight Hours
Total Airframe Cycles:                          37.347 Flight Cycles
C (C05) CHECK:
               Interval:                              5000 / H
               To Go:                                  920 / H   
  Next Scheduled Check due:           23.Feb.2016
 Main Engines (Currently Installed)
Partnumber                             TAY650-15                                     TAY650-15
Time Since New                         48818 / H                                    47777 / H
Cycles Since New                      34984 / C                                    33473 / C
Time Since OH                           24890 / H                                    24934 / H
Cycles Since OH                        17915 / C                                    18194 / C
Last OH Date                          04.Nov.2004                                 21.Jan.2005
Installed Auxiliary Power Unit (APU)
Position                                                              APU
Flight Time Since New                                  25411 / H
Flight Cycles Since New                               34137 / C
Time Since OH                                                   25411 / H
Cycles Since OH                                               34137 / C
Last OH Date
APU Hours Since New                         25.029 / AH (06.Nov.2015)
APU Cycles Since New                        34.358 / AC (06.Nov.2015)
Landing Gears
Position                              Z731                                 Z721                           NLG
Time Since New                    UNKN.                               UNKN.            UNKNOWN
Cycles Since New                30872                            28779                          42711 
Time Since OH                       UNKN.                            UNKN.                         UNKN.
Cycles Since OH                  10944                               10944                       5323 
Last OH Date                  05.Jul.2007                  08.Feb.2007      12.Oct.2010
Next Scheduled Overhaul   593                                 446                           14.677 
Description
Flight Control Computer 1
Flight Control Computer 2
Flight Augmentation Computer
Maintenance Control computer
HF Transceiver
VHF 1 Transceiver
VHF 2 Transceiver
VHF 3 Transceiver
ACARS Management Unit
Digital Cockpit Voice Recorder
Passenger Address
Audio Management Unit
Audio Control Panel 1
Audio Control Panel 2
Audio Control Panel 3
Digital Flight Data Recorder
Flight Data Acquisition Unit
Flight warning computer
MFDU Display 1
MFDU Display 2
Digital Air Data Computer 1
Digital Air Data Computer 2
EFIS Display 1
EFIS Display 2
EFIS Display 3
 F100 PH-ABX msn 11494 delivery for NETWORK PERTH 3 FEB 2012 LES BUSHELL-22015-11-17 12.21.022015-11-17 12.21.292015-11-17 12.24.572015-11-17 12.26.07

Amfibia BE-103 2003

Beriev Be-103                          2003

Przepracował od początku       130h

2 silniki Continental IO-360 ES

Zabiera 4 pasażerów + 2 pilotów.

Zasięg 850km

Pułap 5000m

Wszystkie fotele wyposażone 4 punktowe pasy bezpieczeństwa i kamizelki ratunkowe pod siedzeniem. Siedzenia pasażerów są łatwe do usunięcia dla większej powierzchni bagażowej.

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AN-2V

AN-2V, rok produkcji 1972,  przepracował od początku 11200h, od ostatniego remontu (2008) 180h,  Silnik ASz-62IR 16 seria, rok produkcji 1986, przepracował od początku 1290h, od ostatniego remontu 110h, śmigło AV-2R , rok produkcji 1992, przepracowało 8h, śmigło zapasowe: AV-2, 2 seria, rok produkcji 1980, przepracował od początku 5700h, od ostatniego remontu 250h.

]p1020678 - Kopia12

AN-2

1). Samolot rolniczych An-2, rok 1977, urządzenia do rozpylania (ciecz), urządzenia do siewu (RTSZ-1). Przepracowane godziny 730 h od ostatniego remontu. Łączna liczba godzin 10800 h.

2). Samolot An-2, rok 1978. Przepracowane godziny 430 h od ostatniego remontu. Łączna liczba godzin 11300 h.

3). Samolot An-2, rok 1972. Przepracowane godziny 600 h od ostatniego remontu. Łączna liczba godzin 11800 h.

4). Samolot An-2, rok 1973. Przepracowane godziny 440 h od ostatniego remontu. Łączna liczba godzin 11400 h.